Stitching Technology Reinforced Foam Sandwich Hat Type Reinforced Wall Panel Structure and Its Forming Method

A technology for reinforcing foam and reinforced wall panels is applied in the field of fiber composite material reinforcement, which can solve the problems of easy debonding of foam sandwiches, and achieve the effects of simple manufacturing process, strong bearing capacity and enhanced strength.

Active Publication Date: 2016-07-06
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Abstract
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Problems solved by technology

[0005] The purpose of the present invention is to solve the problem that the foam-reinforced hat-shaped reinforced wall panel and the foam sandwich are easy to debond, and propose a hat-shaped reinforced wall panel that adopts an improved sewing technique to improve the strength, rigidity and stability of the hat-shaped reinforced wall panel. Type-reinforced panel structure and its forming method

Method used

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  • Stitching Technology Reinforced Foam Sandwich Hat Type Reinforced Wall Panel Structure and Its Forming Method
  • Stitching Technology Reinforced Foam Sandwich Hat Type Reinforced Wall Panel Structure and Its Forming Method
  • Stitching Technology Reinforced Foam Sandwich Hat Type Reinforced Wall Panel Structure and Its Forming Method

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Embodiment Construction

[0026] The embodiments of the present invention will be described in further detail below with reference to the accompanying drawings.

[0027] figure 1 Shown is the structure diagram of the prior art, figure 2 Shown is a schematic cross-sectional view of the structure of the present invention, image 3 Shown is a schematic cross-sectional view of the structure of the present invention along the direction of the ribs, where the reference signs are: hat-shaped rib 1, skin 2, foam core material 3, suture 4.

[0028] Such as Figure 1 to Figure 3 As shown, the stitching technology of the present invention enhances the foam sandwich hat-shaped stiffened wall panel structure, including a hat-shaped rib 1 and a skin 2. The hat-shaped rib 1 is fixed on the skin 2 and the hat-shaped rib 1 and the cover A cavity is formed between the skins 2 and the cavity is filled with a foam core material 3, wherein: the hat-shaped stiffened wall structure passes through the hat-shaped rib 1, the foam c...

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Abstract

The invention relates to an improved suture technique enhanced foam sandwich hat stiffened wall panel structure and a forming method thereof, belonging to the technical field of fiber composite enhancement. The foam sandwich hat stiffened wall panel structure is characterized in that the suture technique is used for the foam sandwich hat stiffened wall panel and is used for improving the strength and stiffness of the hat stiffened wall panel. The method comprises the following steps: firstly, laying hat ribs and skin on a stiffened wall panel mould; secondly, perforating a foam core material along the thickness direction according to the pre-designed perforation pattern (the perforation directions of front and rear rows are symmetric along the vertical foam centerline) in a foam sandwich; thirdly, suturing upper and lower panels and the core material with a suture together; finally, combining and packaging the hat ribs, and solidifying. The strength, stiffness and stability of the composite hat stiffened wall panel structure are obviously improved. According to the bearing capacity required by the enhanced hat stiffened wall panel, the suture parameter meeting the requirement can be designed. The suture foam sandwich structure provided by the invention has the advantages of strong bearing capacity, simple manufacturing process, high structural efficiency and low manufacturing and maintenance cost.

Description

Technical field [0001] The invention belongs to the technical field of fiber composite material reinforcement, and particularly relates to a foam sandwich hat-shaped stiffened wall panel structure using an improved stitching technology and a molding method thereof. Background technique [0002] The composite hat-shaped stiffened wall panel structure is widely used in aerospace structures due to its good post-buckling load-bearing capacity, high specific stiffness, good structural stability, high efficiency in transferring circumferential loads, and good weight reduction effects. The first choice for cylindrical structural components such as the fuselage section of large passenger commercial aircraft. [0003] However, an elongated cavity structure is formed between the hat-shaped ribs and the skin, thereby reducing the stability of the hat-shaped stiffened wall panel. At present, some scholars fill the cavities of hat-shaped stiffened wall panels with foam to improve the flexural ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B29C65/62B29C69/00B64C1/12
Inventor 李勇还大军李吻肖军
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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